Methods for the controlled reduction of turbine nozzle flow areas and turbine nozzle components having reduced flow areas
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[0014]The following Detailed Description is merely exemplary in nature and is not intended to limit the invention or the application and uses of the invention. Furthermore, there is no intention to be bound by any theory presented in the preceding Background or the following Detailed Description. Terms such as “comprise,”“include,”“have,” and variations thereof are utilized herein to denote non-exclusive inclusions. Such terms may thus be utilized in describing processes, articles, apparatuses, and the like that include one or more named steps or elements, but may further include additional unnamed steps or elements.
[0015]FIG. 1 is a flowchart illustrating an exemplary method 10 for reducing the effective flow area of a turbine nozzle component. The term “turbine nozzle component” is utilized herein to denote a turbine nozzle segment or other structure that can be mechanically attached to one or more additional components to produce a completed turbine nozzle assembly, such as a tur...
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